CN105477890A - Water-air-amphibious remote control aircraft - Google Patents
Water-air-amphibious remote control aircraft Download PDFInfo
- Publication number
- CN105477890A CN105477890A CN201610006324.5A CN201610006324A CN105477890A CN 105477890 A CN105477890 A CN 105477890A CN 201610006324 A CN201610006324 A CN 201610006324A CN 105477890 A CN105477890 A CN 105477890A
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- CN
- China
- Prior art keywords
- cabin
- water
- aircraft
- compartment
- screw propeller
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
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Classifications
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- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
- A63H27/02—Model aircraft
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- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H27/00—Toy aircraft; Other flying toys
- A63H27/14—Starting or launching devices for toy aircraft; Arrangements on toy aircraft for starting or launching
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- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H29/00—Drive mechanisms for toys in general
- A63H29/10—Driving mechanisms actuated by flowing media
- A63H29/14—Driving mechanisms actuated by flowing media by a water stream
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- A—HUMAN NECESSITIES
- A63—SPORTS; GAMES; AMUSEMENTS
- A63H—TOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
- A63H29/00—Drive mechanisms for toys in general
- A63H29/22—Electric drives
Abstract
The invention provides a water-air-amphibious remote control aircraft which comprises an upper main blade, a lower main blade, a balance rod, a tail rod provided with a tail blade and an aircraft body. The middle of the aircraft body is provided with a watertight bulkhead which divides the aircraft body into a flight compartment and an underwater compartment from top to bottom; the underwater compartment is internally provided with a front compartment body, a middle compartment body and a rear compartment body in sequence from front to rear, and the rear compartment body is externally provided with a rear screw propeller, a left screw propeller and a right screw propeller; the rear compartment body is airtight and provided with a rear motor set, a left motor set and a right motor set, and front-back movement and left-right movement of the remote control aircraft in water are achieved by driving the rear screw propeller, the left screw propeller and the right screw propeller through transmission; the middle compartment body is airtight and provided with a central control board and a battery for providing control and power; the front compartment body is internally provided with a water pump, and water pumping and drainage are achieved through a drain hole under the water pump; the underwater compartment is provided with an exchange hole capable of being closed and allowing a rubber pipe to be inserted therein.
Description
Technical field
The present invention relates to remote control boat aircraft technology field, the telecontrolled aircraft that specifically a kind of water is empty amphibious.
Background technology
At present, along with the development of society and the progress of aeronautical technology, the development of model plane also receives the concern of personages of various circles of society, and market has occurred various aeromodelling airplane, extremely people like.The telecontrolled aircraft of selling in the market, can only realize single flight function, the patent No. be 201330433379.1 this section of patent be exactly like this.People expect can to realize more doing more physical exercises the telecontrolled aircraft of function.
Summary of the invention
The problem to be solved in the present invention is to provide a kind of telecontrolled aircraft in airflight, water with sink-float three kinds of functions in navigation and water.
In order to overcome the above problems, the present invention is achieved through the following technical solutions:
The empty amphibious telecontrolled aircraft of a kind of water, comprise upper and lower main lobe, balancing pole, the foot piece with caudal lobe and fuselage body, its feature is, is provided with watertight bulkhead at the middle part of this fuselage body, fuselage body is divided into cabin in flight cabin and water from top to bottom;
The battery case controlling mainboard, motor and place for lithium battery is provided with in described flight capsule indoor, described control mainboard, motor and confession lithium battery form close access, described motor by gear drive, drives upper and lower two main lobves and balancing pole to rotate, thus provides lift for telecontrolled aircraft; Be provided with at the afterbody in described flight cabin the hole be in communication with the outside, stretch out for foot piece, the one end with caudal lobe outside, by the acting in conjunction of caudal lobe and upper and lower main lobe, realizes travelling forward of aircraft;
Before described water middle deck indoor are provided with from front to back successively, there are rear screw shaft and left-and-right spiral oar in cabin, middle cabin and rear cabin in rear deck outdoor mounted; Described rear cabin watertight, and be provided with rear groups of motors and left and right groups of motors, drive rear screw shaft and left-and-right spiral oar by transmission, realize the front and back in water and side-to-side movement; Described middle cabin watertight, and be provided with middle control mainboard and battery, control and electric power are provided; Described front deck indoor are placed with water pump, by immediately below osculum realize water-pumping/draining; In described water, cabin is provided with closable exchange hole, inserts for rubber tube.
Compared with prior art, the invention has the beneficial effects as follows: due to the structure in cabin in the water of telecontrolled aircraft, under the acting in conjunction of rear screw shaft, left-and-right spiral oar, water pump and control mainboard, the present invention can realize advancing in water, retreat, turn and the motor function of floating dive in left and right.Compensate for the deficiency that prior art can only realize single aerial sports function, achieve the telecontrolled aircraft design that water is empty amphibious.Meanwhile, this telecontrolled aircraft structure is comparatively simple, convenient disassembly.
Accompanying drawing explanation
Fig. 1 is the front view of the empty amphibious telecontrolled aircraft of water of the present invention;
Fig. 2 is the cross section view of the empty amphibious telecontrolled aircraft of water of the present invention;
Fig. 3 is the left side view of the empty amphibious telecontrolled aircraft of water of the present invention;
Fig. 4 is the top view of the empty amphibious telecontrolled aircraft of water of the present invention;
Fig. 5 is the isometric view of the empty amphibious telecontrolled aircraft of water of the present invention.
Detailed description of the invention
Below in conjunction with accompanying drawing, embodiments of the invention are elaborated: the present embodiment is implemented under premised on technical solution of the present invention, give concrete implementation method, but protection scope of the present invention is not limited to following embodiment.
In exemplified by Fig. 2, the empty amphibious telecontrolled aircraft of a kind of water, comprises upper and lower main lobe 5, balancing pole 6, the foot piece with caudal lobe 7 and fuselage body.Described fuselage has flight cabin 1, cabin 2 in water.In described water, cabin is placed in below described flight cabin, and centre separates with watertight bulkhead.
Described flight cabin 1 is built-in with battery case 12, for putting lithium battery, provides electric power.Battery in aerial control mainboard 3, motor 4 and battery case 12 forms close access.Left and right two motors 4 pass through gear drive, drive upper and lower two main lobves 5 and balancing pole 6 to rotate, thus provide lift for telecontrolled aircraft, realize the rise and fall campaign of telecontrolled aircraft, by changing the rotating speed of two motors, the skyborne left-right rotation of aircraft can be realized.Described flight cabin 1 is in communication with the outside afterbody is porose, and foot piece passing hole is stretched out, and has caudal lobe 7 above.By the acting in conjunction of caudal lobe 7 with upper and lower main lobe 5, travelling forward of aircraft can be realized.
In described water, cabin 2 is built-in with front cabin 14, middle cabin 13, rear cabin 11.Described rear cabin watertight, and put rear groups of motors and left and right groups of motors, drive rear screw shaft 9 and left-and-right spiral oar 10 by transmission, realize the front and back in water and side-to-side movement.Described middle cabin 13 watertight, puts in water and controls mainboard and battery, provides control and electric power.Water pump is put in described front cabin 14, by immediately below osculum realize the effect of water-pumping/draining.With a rubber tube and contact air when exchange hole 8 is in water, when draining for water in cabin 2 enough air are provided.By the effect of the water pump in front cabin 14 and exchange hole 8, the motion that the floating in water is sunk just can be realized.
More than describe preferred embodiment of the present invention in detail.Those skilled in the art it should be understood that without departing from the present invention, design according to the present invention can make many modifications and variations.Therefore, all technical staff in the art, all should by the determined protection domain of claims under this invention's idea on the basis of existing technology by changing material or the available technical scheme of feature situation.
Claims (1)
1. the empty amphibious telecontrolled aircraft of water, comprise upper and lower main lobe (5), balancing pole (6), the foot piece with caudal lobe (7) and fuselage body, it is characterized in that, be provided with watertight bulkhead at the middle part of this fuselage body, fuselage body be divided into cabin (2) in flight cabin (1) and water from top to bottom;
The battery case (12) controlling mainboard (3), motor (4) and place for lithium battery is provided with in described flight cabin (1), described control mainboard (3), motor (4) and confession lithium battery form close access, described motor (4) passes through gear drive, drive upper and lower two main lobves (5) and balancing pole (6) to rotate, thus provide lift for telecontrolled aircraft; The hole be in communication with the outside is provided with at the afterbody in described flight cabin (1), stretch out for foot piece, the one end with caudal lobe (7) outside, by the acting in conjunction of caudal lobe (7) with upper and lower main lobe (5), realizes travelling forward of aircraft;
In described water, in cabin (2), be provided with front cabin (14), middle cabin (13) and rear cabin (11) from front to back successively, rear screw shaft (9) and left-and-right spiral oar (10) are installed outside rear cabin (11); Described rear cabin (11) watertight, and be provided with rear groups of motors and left and right groups of motors, drive rear screw shaft (9) and left-and-right spiral oar (10) by transmission, realize the front and back in water and side-to-side movement; Described middle cabin (13) watertight, and be provided with middle control mainboard and battery, control and electric power are provided; Be placed with water pump in described front cabin (14), by immediately below osculum realize water-pumping/draining; In described water, cabin (2) are provided with closable exchange hole (8), insert for rubber tube.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610006324.5A CN105477890B (en) | 2016-01-06 | 2016-01-06 | A kind of empty amphibious telecontrolled aircraft of water |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610006324.5A CN105477890B (en) | 2016-01-06 | 2016-01-06 | A kind of empty amphibious telecontrolled aircraft of water |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105477890A true CN105477890A (en) | 2016-04-13 |
| CN105477890B CN105477890B (en) | 2017-10-20 |
Family
ID=55665383
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610006324.5A Active CN105477890B (en) | 2016-01-06 | 2016-01-06 | A kind of empty amphibious telecontrolled aircraft of water |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105477890B (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106926654A (en) * | 2017-02-22 | 2017-07-07 | 浙江大学 | A kind of amphibious four rotor wing unmanned aerial vehicle |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE675751C (en) * | 1938-02-03 | 1939-05-16 | Dornier Werke Gmbh | Hull for flying boats |
| CN2201975Y (en) * | 1993-01-05 | 1995-06-28 | 徐自毅 | Toy aircraft with electric propellers |
| CN2506541Y (en) * | 2001-07-30 | 2002-08-21 | 罗专予 | Ditachable water sealed cabin for airplane |
| CN201686008U (en) * | 2010-04-02 | 2010-12-29 | 黄建华 | Deep-sea tourism submarine |
| ES1077959U (en) * | 2012-10-17 | 2012-11-02 | Domingo Bengoa Saez De Cortazar | Water storage device for aircraft (Machine-translation by Google Translate, not legally binding) |
| CN205340144U (en) * | 2016-01-06 | 2016-06-29 | 上海交通大学 | Empty amphibious telecontrolled aircraft of water |
-
2016
- 2016-01-06 CN CN201610006324.5A patent/CN105477890B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE675751C (en) * | 1938-02-03 | 1939-05-16 | Dornier Werke Gmbh | Hull for flying boats |
| CN2201975Y (en) * | 1993-01-05 | 1995-06-28 | 徐自毅 | Toy aircraft with electric propellers |
| CN2506541Y (en) * | 2001-07-30 | 2002-08-21 | 罗专予 | Ditachable water sealed cabin for airplane |
| CN201686008U (en) * | 2010-04-02 | 2010-12-29 | 黄建华 | Deep-sea tourism submarine |
| ES1077959U (en) * | 2012-10-17 | 2012-11-02 | Domingo Bengoa Saez De Cortazar | Water storage device for aircraft (Machine-translation by Google Translate, not legally binding) |
| CN205340144U (en) * | 2016-01-06 | 2016-06-29 | 上海交通大学 | Empty amphibious telecontrolled aircraft of water |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106926654A (en) * | 2017-02-22 | 2017-07-07 | 浙江大学 | A kind of amphibious four rotor wing unmanned aerial vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105477890B (en) | 2017-10-20 |
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